View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 36595U 10026A 10177.95752728 .32171212 75409-6 37788-3 0 9994
2 36595 034.4831 240.6410 0001391 255.6829 104.5617 16.50051425 3591
| Epoch (UTC): | 26 June 2010 22:58:50 |
| Eccentricity: | 0.0001391 |
| inclination: | 34.4831° |
| perigee height: | 138 km |
| apogee height: | 140 km |
| right ascension of ascending node: | 240.6410° |
| argument of perigee: | 255.6829° |
| revolutions per day: | 16.50051425 |
| mean anomaly at epoch: | 104.5617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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